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An investigation of a full-scale advancing blade concept rotor system at high advance ratioWind tunnel tests of full scale advancing blade concept rotor system at high advance ratio
Document ID
19710024041
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Falarski, M. D. (Army Air Mobility Research and Development Lab. Moffett Field, CA, United States)
Mc Cloud, J. L. (Army Air Mobility Research and Development Lab. Moffett Field, CA, United States)
Soderman, P. T. (Army Air Mobility Research and Development Lab. Moffett Field, CA, United States)
Stroub, R. H. (Army Air Mobility Research and Development Lab. Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
August 1, 1971
Subject Category
Aircraft
Report/Patent Number
NASA-TM-X-62081
Report Number: NASA-TM-X-62081
Accession Number
71N33517
Funding Number(s)
CONTRACT_GRANT: 721-60-10-02-00-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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